Timothy R. Moes

• A preliminary look at techniques used to obtain airdata from flight at high angles of attack
• Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
• Flight demonstration of a shock location sensor using constant voltage hot-film anemometry
• In-flight investigation of shuttle tile pressure orifice installations
• Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flights
• Wind-tunnel development of an SR-71 aerospike rocket flight test configuration